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Research Article Open access CC BY 4.0

Material Selection for Gas Turbine Blade Coating Using GRANTA Material Selector

A. A. Abioye, P. O. Atanda, S. B. Majolagbe, D. A. Isadare, O. P. Abioye, K. J. Akinluwade, A. R. Adetunji

Advances in Research · pp. 1–9 · Published 26 May 2015

10.9734/AIR/2015/15769

Abstract

This paper presents the selection of suitable candidate materials for thermal barrier coating of gas turbine blade using GRANTA software. There have been reported cases of gas turbine blade failure in service due to the extreme service conditions. Such failure could possibly have occurred due to poor material selection for thermal barrier coatings on the turbine blade thereby exposing the blade to harsh condition over time. The major adverse effects on these blades are thermal fatigue, high temperature oxidation, hot corrosion, interdiffusion, high cycle fatigue and creep.  

Thermal fatigue turbine blade oxidation corrosion interdiffusion fatigue creep barrier coatings GRANTA

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